Call Number (LC) Title Results
Y 3.N 21/5:6/2546 Viscosities of air and nitrogen at low pressures / 1
Y 3.N 21/5:6/2547 An investigation by the hodograph method of flow through a symmetrical nozzle with locally supersonic regions / 1
Y 3.N 21/5:6/2548 Equal-strength design of tension-field webs and uprights / 1
Y 3.N 21/5:6/2549 Investigation of hydrocarbon ignition / 1
Y 3.N 21/5:6/2550 Determination of shapes of boattail bodies of revolution for minimum wave drag / 1
Y 3.N 21/5:6/2551 Effect of various parameters including Mach number on the single-degree-of-freedom flutter of a control surface in potential flow / 1
Y 3.N 21/5:6/2552 Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow / 1
Y 3.N 21/5:6/2553 Pitching-moment derivatives Cmq and Cma at supersonic speeds for a slender-delta-wing and slender-body combination and approximate solutions for broad-delta-wing and slender-body combinations / 1
Y 3.N 21/5:6/2554 Theoretical aerodynamic characteristics of a family of slender wing-tail-body combinations / 1
Y 3.N 21/5:6/2555 Effect of taper ratio on the low-speed rolling stability derivatives of swept and unswept wings of aspect ratio 2.61 / 1
Y 3.N 21/5:6/2556 Buckling of rectangular sandwich plates subjected to edgewise compression with loaded edges simply supported and unloaded edges clamped / 1
Y 3.N 21/5:6/2557 Infrared spectra of 59 dicyclic hydrocarbons / 1
Y 3.N 21/5:6/2558 Some effects of variables in several parameters including fluid density on the flutter speed of light uniform cantilever wings / 1
Y 3.N 21/5:6/2559 Theoretical and experimental investigation of condensation of air in hypersonic wind tunnels / 1
Y 3.N 21/5:6/2560 An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer / 1
Y 3.N 21/5:6/2561 A study of Poisson's ratio in the yield region / 1
Y 3.N 21/5:6/2562 Numerical determination of indicial lift of a two-dimensional sinking airfoil at subsonic Mach numbers from oscillatory lift coefficients with calculations for Mach number 0.7 / 1
Y 3.N 21/5:6/2563 Experimental investigation of rolling performance of straight and sweptback flexible wings with various ailerons / 1
Y 3.N 21/5:6/2564 Properties of honeycomb cores as affected by fiber type, fiber orientation, resin type, and amount / 1
Y 3.N 21/5:6/2565 A theoretical analysis of the effect of several auxilliary damping devices on the lateral stability and controllability of a high-speed aircraft / 1